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Effects of the Reynolds number and structural damping on vortex-induced vibrations of elastically-mounted rigid cylinder

机译:雷诺数和结构阻尼对弹性安装刚性圆柱涡流振动的影响

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摘要

In this work, analyses of the damping ratio and turbulence effects on three-dimensional vortex-induced vibrations of a two degrees-of-freedom elastically mounted rigid cylinder are carried out. Simulations are conducted for damping ratios of zeta = 0.5, 2.5, 5.0 and 10.0% for flows covering Reynolds numbers in the three TrSL flow regimes, in the range of Re = 7.5 x 10(2) to 1.3 x 10(5). Variation of the response amplitudes, phase angles, force coefficients and frequency ratios by the damping ratios and Reynolds number are investigated using the classically damped spring-mass system equations programmed inside the CFD software Fluent. New results are obtained for very high Reynolds numbers and different damping ratios. New conclusions are drawn from the mechanical responses using surface interpolation of 240 data-points, which allows the investigation of the trends of a given response variable xi based on the A(gamma)*vs.zeta((m* + C-A) vs. xi three-dimensional plot proposed by the authors. A new mechanism of elongation of the upper branch extension based on the universal reduced damping, S-u, during the TrSL3 regime is described.
机译:在这项工作中,进行了对两个自由度的三维涡旋诱导的三维涡旋诱导振动的阻尼比和湍流效应的分析。对于覆盖三个TRSL流动制造规范的雷诺数的流动的流量,Zeta = 0.5,2.5,5.0和10.0%的阻尼比进行模拟,在RE = 7.5×10(2)至1.3×10(5)的范围内。使用CFD软件流畅的CFD软件中的经典阻尼的弹簧质量系统方程来研究响应幅度,相位角,力系数和频率比的变化。获得非常高的雷诺数和不同阻尼比的新结果。使用240个数据点的表面插值来从机械响应中得出新的结论,这允许基于A(Gamma)* zeta((m * + ca)与其对给定响应变量xi的趋势进行调查描述了作者提出的三维情节。描述了基于TRSL3制度的通用降低阻尼的上分支延伸的新机制。

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